隧道波导环境中旋翼飞行器姿态控制方法研究  

Research on attitude control method of rotorcraft in tunnel waveguide environment

作　　者：何光华 黄薛凌 徐雅惠 齐金龙 周宇丰 HE Guanghua;HUANG Xueling;XU Yahui;QI Jinlong;ZHOU Yufeng(Wuxi Electric Power Supply Company,State Grid Jiangsu Electric Power Co.,Ltd.,Wuxi 214000,China)

机构地区：[1]国网江苏省电力有限公司无锡供电分公司,江苏无锡214000

出　　处：《电子设计工程》2023年第9期59-62,67,共5页Electronic Design Engineering

基　　金：国网江苏省电力有限公司科技项目资助(J2020094)。

摘　　要：目前研究的旋翼飞行器姿态控制方法在隧道波导环境下控制精度较低,鲁棒性较差。为了解决上述问题,针对隧道波导环境研究了一种新的旋翼飞行器姿态控制方法。分析狭窄隧道环境下旋翼飞行器湍流的形成,研究飞机在飞行器湍流形成过程中的层流失稳、转捩与进入湍流发展状态。确定雷诺数,计算旋翼飞行器转捩位置,根据紊流尺度得到雷诺数。采用PCS对偏航通道、俯仰、滚转进行姿态控制,使旋翼飞行器可稳定、安全飞行。实验结果表明,研究的旋翼飞行器姿态控制方法具有较强的分析系统动态性能的能力,可以在隧道波导环境中保持良好的控制性能的能力,提高了鲁棒性。The attitude control method of rotorcraft studied at present has low control accuracy and poor robustness in tunnel waveguide environment.In order to solve the above problems,a new attitude control method for rotorcraft in tunnel waveguide environment is studied.This paper analyzes the formation of turbulence of rotorcraft in narrow tunnel environment,and studies the state of aircraft:laminar instability,transition and entering the development state of turbulence.Determine the Reynolds number,calculate the transition position of rotorcraft,and obtain the Reynolds number according to the turbulence scale.PCS is used to control the attitude of yaw channel,pitch and roll,so that the rotorcraft can fly stably and safely.The experimental results show that the rotor aircraft attitude control method has strong analysis system dynamic performance,can maintain good control performance and improve robustness in tunnel waveguide environment.

关 键 词：隧道波导环境 旋翼飞行器 姿态控制 控制方法 飞行器姿态 

分 类 号：V448[航空宇航科学与技术—飞行器设计]